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QPS requirements

Information

Jkt 247047

Test

FTD level
Tolerances

1.j.4. .......................

Autorotational Landing ..

2.

Handling Qualities

2.a. ........................

Control System Mechanical Characteristics.

Contact the NSPM for clarification
of any issue regarding helicopters with reversible controls.

2.a.1. .....................

Cyclic .............................

Breakout - Section0.25 lbs (0.112 daN)
or 25%. Force - Section1.0 lb (0.224
daN) or 10%.

Flight conditions

Test details

Notes
5

Frm 00456

Torque - Section3%, Rotor Speed - 
Section3%, Vertical Velocity - Section100
fpm (0.50 m/sec) or 10%, Pitch
Attitude - Section2Section, Bank Attitude - 
Section2Section, Heading - Section5Section, Longitudinal Control Position - Section10%,
Lateral
Control
Position - 
Section10%, Directional Control Position - Section10%, Collective Control
Position - Section10%.

Sfmt 8002
Q:\14\14V2.TXT
PC31

Record the results of an
autorotational deceleration and
landing from a stabilized
autorotational descent, to touch
down.

Ground; Static conditions. Trim On and
Off. Friction Off.
Augmentation On
and Off.

Record results for an uninterrupted control sweep to the
stops. (This test does not apply
if aircraft hardware modular
controllers are used.).

7
X

446

Fmt 8010

Landing .....................

6

X

X

X

If flight test data containing
all required parameters
for a complete power-off
landing is not available
from the aircraft manufacturer for this test, and
other qualified flight test
personnel are not available to acquire this data,
the sponsor must coordinate with the NSPM to
determine if it would be
appropriate to accept alternative testing means.
Alternative approaches to
this data acquisition that
may be acceptable are:
(1) A simulated
autorotational flare and
reduction of rate of descent (ROD) at altitude;
or (2) a power-on termination following an
autorotational approach
and flare.

14 CFR Ch. I (1-1-19 Edition)

Title

PO 00000

Entry No.

Pt. 60, App. D

16:30 Jun 25, 2019

TABLE D2A - FLIGHT TRAINING DEVICE (FTD) OBJECTIVE TESTS - Continued